| The B 634 represented the ultimate in the aerodynamic
development of the basic B 34 single-seat fighter
biplane design, and was to be numbered among the
cleanest aircraft in its category ever flown. Tested in
1936, the B 634 was powered by an Avia-built HS
12Ycrs engine mounting a 20mm Oerlikon FFS cannon,
two 7.7mm Model 30 machine guns being installed in
the upper fuselage decking. There was virtually no
commonality of components between the B 634 and the
B 534.1 from which it was derived. By comparison with
the earlier fighter, the upper wing of the B 634 featured
increased chord while the lower wing had reduced
chord, the wingtips were redesigned, the ailerons were
broader, the gap was reduced (increasing the splay of
the interplane struts), the stagger was greatly increased,
and cut-outs were introduced on the lower
wing roots. The curvature of the engine cowling and
cockpit sill was refined, cantilever undercarriage legs
were adopted and the radiator bath was faired cleanly between the leg roots. Despite a substantial reduction
in drag, performance offered an insufficient improvement
over that of the B 534 to warrant series production,
the disappointing results provided by the B 634
being due primarily to a substantial increase in structural
weight.
| A three-view drawing (1633 x 1230) |
MODEL | B.634 |
CREW | 1 |
ENGINE | 1 x 850hp Avia-Hispano Suiza 12Ycrs |
WEIGHTS |
Take-off weight | 2340 kg | 5159 lb |
Empty weight | 1710 kg | 3770 lb |
DIMENSIONS |
Wingspan | 9.40 m | 31 ft 10 in |
Length | 8.35 m | 27 ft 5 in |
Height | 3.06 m | 10 ft 0 in |
PERFORMANCE |
Max. speed | 415 km/h | 258 mph |
Cruise speed | 362 km/h | 225 mph |
Ceiling | 11000 m | 36100 ft |
Rate of climb | 960 m/min | 3150 ft/min |
Range | 500 km | 311 miles |
ARMAMENT | 1 x 20mm, 2 x 7.7mm |
Psellos, e-mail, 25.10.2010 01:32 Two prototypes built - second one different than the one shown here. It had enclosed canopy and different undercarige. Both B-634 were pressed to service in 1938. reply |
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